Aerodynamics and aero-acoustics of rectangular planform cavities. Part II: Unsteady flow and aero-acoustics.
Abstract:The information given in ESDU 04023 concerns unsteady flow and the associated aero-acoustics of rectangular planform cavities. Following a general introduction concerning the ranges of cavity geometry over which sustained oscillations can be expected, the three oscillation types, i.e. fluid-dynamic, fluid-resonant - including the special case of normal mode resonance, and fluid-elastic, as suggested by Rockwell and Naudascher, are discussed together with the various mechanisms involved. The parameters that can affect the frequency and amplitude of cavity oscillations for the important fluid-dynamic and fluid-resonant typesinvolved in aircraft applications are detailed.
The physical processes involved in a length mode fluid-resonant oscillation cycle are discussed. The historical view of the oscillation process as suggested by the classical work of Rossiter, Bilanin andCovert, Heller and Bliss, Rockwell and Naudascher, with later work by Heller and Delfs, precedes the more detailed analyses made possible by the CFD simulations of Zhang et al., Tam et al. and Henderson.
The various "engineering" methods for the prediction of cavity oscillations are outlined and examined. The range of empirical and analytical methods for predicting tonal frequencies in length mode, including thewidely used modified form of Rossiter's method are presented. So is a development of East's semi-empirical method for predicting the fundamental depth mode frequency at low speeds, based on the theoretical pressure amplification equation established by the work of Plumblee et al. The new development uses East's simple equation as a basis for the provision of a more general equation providing a fairing between the low width/length ratios covered by Plumblee et al. and the high, quasi-two-dimensional, values for which East's original method was derived. The scope of the available engineering methods for tonal amplitude prediction is limited to that of the Cavity Acoustics Prediction (CAP) Code for length modes and the Plumblee et al. method for depth modes.
Concluding remarks include a list of those areas requiring further information to provide a firmer basis for some of the discussion in the Data Item.
Appendix A contains basic information on the various measures of fluctuating pressure and their analysis.
Appendix B provides further information on OASPL together with approximate methods for its evaluation using acoustic spectra, illustrated by means of three worked examples.
|Data Item ESDU 04023|
- Aircraft Noise
- Fatigue - Endurance Data
- Fatigue - Fracture Mechanics
- Fluid Mechanics, Internal Flow
- Fluid Mechanics, Internal Flow (Aerospace)
- Heat Transfer
- Physical Data, Chemical Engineering
- Stress and Strength
- Transonic Aerodynamics
- Vibration and Acoustic Fatigue
- Wind Engineering